Multi-fidelity model based optimization of shaped film cooling hole and experimental validation-Reference-Cited by-同舟云学术

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Multi-fidelity model based optimization of shaped film cooling hole and experimental validation

Published:2019-04 Issue: Volume:132 Page:118-129
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Zhang Hao,Li Yifei,Chen Ziyu,Su Xinrong,Yuan Xin

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference34 articles.

1. Film cooling of a gas turbine blade;Ito;J. Eng. Power,1978

2. Turbine endwall film cooling with combustor-turbine interface gap leakage flow: effect of incidence angle;Zhang;J. Therm. Sci.,2013

3. Effect of inlet rotating swirl on endwall film cooling for two representative hole arrangements;Zhou;Chin. J. Aeronaut.,2018

4. A novel sand-dune-inspired design for improved film cooling performance;Zhou;Int. J. Heat Mass Transf.,2017

5. Y. Li, Y. Zhang, X. Su, X. Yuan, Experimental and numerical investigations of shaped hole film cooling with the influence of endwall cross flow 120 (2018) doi:https://doi.org/10.1016/j.ijheatmasstransfer.2017.11.150.

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